Research Article
Data Transfer Schemes in Rotorcraft Fluid-Structure Interaction Predictions
Figure 6
Comparison of convergence on section airloads M2Cn at r/R = 0.87 with coupling iterations.
| (a) Method 1 |
| (b) Method 2 |
| (c) Method 3 |
| (a) Method 1 |
| (b) Method 2 |
| (c) Method 3 |